2LiuBJ, YuXJ, Liu HX, et al. Application of SPIVin turbornachineryEJ:. Experiments in Fluids, 2006, 40(4) 621-642.
3Baumgartner M, Karneier F, Hourrnouziadis J. Non-en- gine order blade vibration in a high pressure compressor [C]//20th International Symposium on Airbreathing En- gines, 1995: 1-13.
4Karneier F, Neise W. Rotating blade flow instability as a source of noise in axial turbomachines:J:. Journal of Sound and Vibration, 1997, 203(5) : 833-853.
5M:rz J, Hah C, Neise W, et al. An experimental and nu merical investigation into the mechanisms of rotating insta bility[J]. Journal of Turbomachinery, 2002, 124 (3): 367-375.
6Yu X J, Liu B J. Stereoscopic PIV measurement of un steady flows in an axial compressor stage[J:. Experimen tal Thermal and Fluid Science, 2007, 31(8): 1049-1060.
7Drolet M, Thomassin J, Vo H D, et al. Numerical inves tigation into non-synchronous vibrations of axial flow corn pressors by the resonant tip ings of ASME Turbo Expo clearance flow[C]//Proceed 2009: Power for Land, Seaand Air, 2009: 487-498.
8Kameier F, Neise W. Rotating blade flow instability as a source of noise in axial turbomachinesEJ:. Journal of Sound and Vibration, 1997, 203(5): 722-742.
9Vignau-Tuquet F, Girardeau D. Aerodynamic rotating vortex instability in a multi-stage axial compressor[C]// 17th International Symposium on Airbreathing Engines, 2005 : 1-8.
10Kikuta H, lwakir K, Furukawa M, et al. Unsteady and three-dimensional flow mechanism of spike-type stall in- ception in an axial flow compressor rotor[C]//ASME JSME-KSME 2011 Joint Fluids Engineering Conference, 2011: 817-829.